# Service difficulty reports: N602AL, cancelled May 29, 2014 A list on [N602AL, cancelled May 29, 2014](https://openairdocs.org/deregistered/N602AL-2014-05-29.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 8 · 377 reports - [SDR IXXA110082O](https://openairdocs.org/sdr/IXXA110082O.md): Connector · loose · Dec 21, 2011 · N602AL · Doug DC873F · Landing Gear System Wiring > DURING UPLATCH CHECK, DOOR NOT LATCH LIGHT CAME ON. THE CREW CYCLED MAIN GEARS TWICE AND DOOR NOT LATCH LIGHT REMAINED ON. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MAIN GEAR DOORS AND FOUND THE LT GEAR DOOR SWITCH CONNECTOR LOOSE AND DIRTY. M - [SDR IXXA110081O](https://openairdocs.org/sdr/IXXA110081O.md): Connector · dirty · Dec 20, 2011 · N602AL · Doug DC873F · Landing Gear System Wiring > DURING CLIMB OUT, AFTER GEAR RETRACTION, DOOR NOT LATCH LIGHT REMAINED ON. CREW CYCLED MAIN GEAR AND LIGHT REMAINED ON. LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MAIN GEAR DOOR UPLATCH SWITCHES AND FOUND THE RT MAIN GEAR DOOR SWITCH CONNECTOR DIRTY. CLEA - [SDR IXXA110037O](https://openairdocs.org/sdr/IXXA110037O.md): Control Tube · dirty · May 5, 2011 · N602AL · Doug DC873F · Engine (Turbine/Turboprop) > AT FLIGHT LEVEL 370, THE NR 2 ENGINE POWER ROLLED BACK FROM 94 PERCENT TO 87 PERCENT WITH A CORRESPONDING DROP IN EGT AND N2. THE PMC FOR NR 2 ENGINE WAS SWITCH OFF AND NR 2 ENG ROLLED DOWN MORE TO 50 PERCENT N1 AND 400 DEGREE EGT. THE CREW SHUTDOWN NR 2 ENGIN - [SDR IXXA110024O](https://openairdocs.org/sdr/IXXA110024O.md): Wheel · dirty · Feb 22, 2011 · N602AL · Doug DC873F · Wheel/Ski/Float > DURING TAKE OFF ROLL THE CREW HAD NO DIRECTIONAL CONTROL OF AIRCRAFT, THE CREW ABORTED TAKEOFF AND THE AIRCRAFT CAME TO A REST WITH THE NOSE GEAR OFF THE RUNWAY. THE AIRCRAFT WAS TOWED BACK TO BLOCKS. MAINTENANCE ACCOMPLISHED REJECTED TAKEOFF INSPECTION, REPLA - [SDR IXXA110007O](https://openairdocs.org/sdr/IXXA110007O.md): Control Valve · defective · Jan 22, 2011 · N602AL · Doug DC873F · Landing Gear Retraction/Extension System > DURING CRUISE, DOOR NOT LATCHED, RED LIGHT ON WITH GEAR UP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED LT MLG DOOR CONTROL VALVE. OPS CHECK GOOD IAW MM 32-32-7. ACFT WAS RETURNED TO SERVICE. - [SDR IXXA110002O](https://openairdocs.org/sdr/IXXA110002O.md): Mechanism · out of adjust · Jan 13, 2011 · N602AL · Doug DC873F · Landing Gear Position and Warning > DURING CLIMB OUT, THE DOOR NOT LATCH LIGHT CAME ON WITH GEAR RETRACTED. THE CREW CYCLED AND ACCOMPLISHED UPLATCH CHECK AND DOOR NOT LATCH LIGHT REMAINED ON. THEY RETURNED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND LT MAIN LANDING GEAR FOLLOW UP MECHANI - [SDR IXXA110001O](https://openairdocs.org/sdr/IXXA110001O.md): Warning Switch · arced · Jan 12, 2011 · N602AL · Doug DC873F · Landing Gear Position and Warning > DURING CLIMB OUT, THE "DOOR NOT LATCH" LIGHT CAME ON WITH LANDING GEAR RETRACTED. THE CREW CYCLED GEAR AND ACCOMPLISHED UPLATCH CHECK, DOOR NOT LATCH LIGHT REMAINED ON THE REMAINDER OF FLIGHT. LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND FLUID CO - [SDR IXXA10SMN114S](https://openairdocs.org/sdr/IXXA10SMN114S.md): Skin · damaged · Nov 13, 2010 · N602AL · Doug DC873F · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSP FOUND LT WING T/E LOWER SKIN HAS IMPROPER REPAIR AT STA XW 730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREAT - [SDR IXXA10SMN113S](https://openairdocs.org/sdr/IXXA10SMN113S.md): Fitting · cracked · Nov 11, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 902.000 LONG 19 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-3-1. - [SDR IXXA10SMN112S](https://openairdocs.org/sdr/IXXA10SMN112S.md): Web · cracked · Nov 11, 2010 · N602AL · Doug DC873F · Fuel Storage > DURING ROUTINE C-CHECK INSP FOUND NR 3 MAIN TANK WEB CRACKED AT STATON XRS 168.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP, SHIMS, SPLICES, FILLER, ANGLE, TEE, AND FI - [SDR IXXA10SMN111S](https://openairdocs.org/sdr/IXXA10SMN111S.md): Skin · damaged · Nov 11, 2010 · N602AL · Doug DC873F · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSP FOUND LT WING T/E UPPER SKIN DOUBLER WITH IMPROPER REPAIR AT STA XW 736.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEAN - [SDR IXXA10SMN110S](https://openairdocs.org/sdr/IXXA10SMN110S.md): Spar Cap · cracked · Nov 11, 2010 · N602AL · Doug DC873F · Wing Spar > DURING ROUTINE C-CHECK INSP, FOUND NR 3 MAIN TANK LOWER CTR SPAR CAP AND WEB CRACKED AT STA XRS 168.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP, SHIMS, SPLICES, FILLER - [SDR IXXA110039S](https://openairdocs.org/sdr/IXXA110039S.md): Floor Panel · corroded · Nov 10, 2010 · N602AL · Doug DC873F · Fuselage Floor Panel > DURING ROUTINE C-CK INSP FOUND MAIN CARGO COMPARTMENT FLOOR PANEL SKIN CORRODED BETWEEN STA 1060.000 LT BOTTOM LINE10. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLERS AND FIL - [SDR IXXA10SMN109S](https://openairdocs.org/sdr/IXXA10SMN109S.md): Longeron · corroded · Nov 10, 2010 · N602AL · Doug DC873F · Fuselage Structure (General) > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT AFT SECTION FLOOR LONGERON 36 CORRODED AT STA 1690.000 - 1725.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON AND STRAPS. CLEANED, TREATED, PRIMED ARE - [SDR IXXA10SMN108S](https://openairdocs.org/sdr/IXXA10SMN108S.md): Fitting · cracked · Nov 10, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 781.000, LONGERON 19 & 20 RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SR - [SDR IXXA10SMN107S](https://openairdocs.org/sdr/IXXA10SMN107S.md): Fitting · cracked · Nov 10, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 857.000, LONGERON 19 & 20 RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SR - [SDR IXXA10SMN106S](https://openairdocs.org/sdr/IXXA10SMN106S.md): Fitting · cracked · Nov 10, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 1160.000, LONGERON 20RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53 - [SDR IXXA10SMN105S](https://openairdocs.org/sdr/IXXA10SMN105S.md): Fitting · cracked · Nov 9, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 717.000 LT BOTTOM LINE 22. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-2-0 - [SDR IXXA10SMN104S](https://openairdocs.org/sdr/IXXA10SMN104S.md): Fitting · cracked · Nov 9, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 700.000, LT BOTTOM LINE 23. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53- - [SDR IXXA10SMN103S](https://openairdocs.org/sdr/IXXA10SMN103S.md): Fitting · corroded · Nov 9, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STATION 960.000 - 980.000 RT BOTTOM LINE 28. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51 - [SDR IXXA10SMN102S](https://openairdocs.org/sdr/IXXA10SMN102S.md): Skin · delaminated · Nov 9, 2010 · N602AL · Doug DC873F · Elevator, Plate/Skin > DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR T/E LOWER SKIN CRACKED AND DELAMINATED AT STA XE 77.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED - [SDR IXXA10SMN101S](https://openairdocs.org/sdr/IXXA10SMN101S.md): Skin · cracked · Nov 9, 2010 · N602AL · Doug DC873F · Elevator, Plate/Skin > DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR T/E LOWER SKIN CRACKED AND DELAMINATED AT STA XE 132.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATE - [SDR IXXA10SMN115S](https://openairdocs.org/sdr/IXXA10SMN115S.md): Skin · corroded · Nov 6, 2010 · N602AL · Doug DC873F · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSP FOUND LT WING L/E LOWER PART CORRODED ST STATION XFS 335.250 - 341.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. FABRICATED DOUBLER AND FILLERS. CLEANED, TREA - [SDR IXXA10SMN100S](https://openairdocs.org/sdr/IXXA10SMN100S.md): Skin · broken · Nov 6, 2010 · N602AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C-CHECK INSP, FOUND LT INBD FLAP UPPER SKIN BROKEN AT STA XW 107.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR - [SDR IXXA10SMN099S](https://openairdocs.org/sdr/IXXA10SMN099S.md): Skin · corroded · Nov 6, 2010 · N602AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C-CHECK INSP, FOUND LT OTBD FLAP LOWER SKIN CORRODED AT STA XF 407.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH - [SDR IXXA10SMN098S](https://openairdocs.org/sdr/IXXA10SMN098S.md): Fitting · corroded · Nov 3, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL FRAME FITTING CORRODED AT STATION 879.375, LONGERON 24LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED FITTING. FABRICATED NEW FITTING, SPLICES, DOUBLER AND SHIMS. CLEANED, TREATED, PRIMED AREA - [SDR IXXA10SMN097S](https://openairdocs.org/sdr/IXXA10SMN097S.md): Fitting · cracked · Nov 3, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL FRAME FITTING CRACKED AT STATION 920.000, LONGERON 24 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FITTING. FABRICATED NEW FITTING, SPLICES, FILLERS, AND DOUBLERS. CLEANED, TREATED, PRI - [SDR IXXA10SMN096S](https://openairdocs.org/sdr/IXXA10SMN096S.md): Fitting · cracked · Nov 2, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP, FOUND CRACKED FITTING AT STA 857.000 & 879.000 LONGERON 24LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP DRILL END OF CRACKS. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED INTERNAL AND EXTERNAL D - [SDR IXXA100047O](https://openairdocs.org/sdr/IXXA100047O.md): Fire Loop · defective · Sep 23, 2010 · N602AL · Doug DC873F · Fire Detection > DURING CRUISE, NR 2 ENGINE FIRE WARNING CAME ON AT FL270 SAT -52. THE CREW SHUTDOWN THE NR 2 ENGINE, WHILE PASSING THROUGH 14,000 FT THE ACFT WAS EXPERIENCING SOME TURBULANCE AND NR 2 FIRE WARNING AND SHORT CIRCUIT LIGHTS ILLUMINATED. CREW DISCHARGED BOTH FIR - [SDR IXXA100043O](https://openairdocs.org/sdr/IXXA100043O.md): Sensor · defective · Aug 26, 2010 · N602AL · Doug DC873F · Airspeed/Mach Indicator > DURING TAKEOFF, THE MAX AIRSPEED WARNING LIGHT AND CLACKER CAME ON. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX REPLACED THE OVERSPEED LIMIT SENSOR. OPS CHECK GOOD IAW MM 34-11-0. ACFT WAS RETURNED TO SERVICE. - [SDR IXXA100039O](https://openairdocs.org/sdr/IXXA100039O.md): Indicator · defective · Aug 12, 2010 · N602AL · Doug DC873F · Attitude and Direction Data System > DURING CLIMB OUT, STANDBY ATTITUDE INDICATOR INOPERATIVE, THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED THE STANDBY ATTITUDE INDICATOR. OPS CHECK GOOD IAW MM34-28-0. ACFT WAS RETURNED TO SERVICE. - [SDR IXX2008F00089](https://openairdocs.org/sdr/IXX2008F00089.md): Switch · inoperative · Jul 30, 2008 · N602AL · Doug DC873F · Landing Gear Position and Warning > FLIGHT ATN 802, DURING CRUISE FROM KTOL, GEAR DOOR NOT LATCHED LIGHT CAME ON INTERMITTENT. THE CREW ACCOMPLISHED ABNORMAL CHECK 3-13-01. THE CREW LANDED IN KLAX WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BAD MAIN LANDING DOOR SWITCH. MAINTENANCE REPLACED - [SDR IXX2008F00021](https://openairdocs.org/sdr/IXX2008F00021.md): Connector · damaged · Jul 18, 2008 · N602AL · Doug DC873F · Fire Protection System Wiring > FLT NR: ATN 842/KTOL TO KPHL. DURING CLIMB FROM KTOL THE NR 4 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST AND DISCHARGED BOTH FIRE BOTTLES. THE ACFT LANDED AT KPHL WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 4 ENGINE FIRE DETECTION - [SDR IXX2008F00014](https://openairdocs.org/sdr/IXX2008F00014.md): Fire Warning · illuminated · Jul 18, 2008 · N602AL · Doug DC873F · Fire Detection > DURING CLIMB, THE NR 4 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST AND DISCHARGED BOTH FIRE BOTTLES. THE AC LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN WORK. (K) - [SDR IXX2008F00016](https://openairdocs.org/sdr/IXX2008F00016.md): Fire Detector · malfunctioned · Jul 10, 2008 · N602AL · Doug DC873F · Fire Detection > DURING CRUISE, NR 3 FIRE WARNING CAME ON, THE CREW DISCHARGED BOTH FIRE BOTTLES AND SHUTDOWN NR 3 ENGINE. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RT CORE SENSING ELEMENT, LT AND RT FAN FIRE SENSING ELEMENT, AND BOTH FIRE BOTTLES, OPS CHECK GOO - [SDR IXXA08SMN185S](https://openairdocs.org/sdr/IXXA08SMN185S.md): Floor Panel · corroded · May 7, 2008 · N602AL · Doug DC873F · Fuselage Floor Panel > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FLOOR PANEL WITH CORROSION AT STATION 1425.000 RIGHT BOTTOM LINE 50. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DO - [SDR IXXA08SMN184S](https://openairdocs.org/sdr/IXXA08SMN184S.md): Cargo Track · worn · Apr 24, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 6 TRACK WITH LUG WORN AT STATION 1580.000. REMOVED EXISTING SPLICES (AFT SIDE). REMOVED SEGMENT OF DAMAGED TRACK. FABRICATED NEW SPLICES. CLEANED, TREATED AND PRIMED AREA, AND EXISTING - [SDR IXXA08SMN138S](https://openairdocs.org/sdr/IXXA08SMN138S.md): Skin · cracked · Apr 17, 2008 · N602AL · Doug DC873F · Wing, Plate/Skin > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 STUB WING DOUBLER SHOWS CRACK AT STATION XS 515.720. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW EXTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND - [SDR IXXA08SMN137S](https://openairdocs.org/sdr/IXXA08SMN137S.md): Cargo Track · worn · Apr 17, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 680.000. REMOVED EXISTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK AFT SIDE. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND SPL - [SDR IXXA08SMN136S](https://openairdocs.org/sdr/IXXA08SMN136S.md): Cargo Track · broken · Apr 17, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 2 TRACK WITH LUGS, BROKEN AT STATION 55.000. REMOVED SEGMENT OF DAMAGED TRACK AND EXITING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXITING SPLICES. INSTALLED NEW TRACK AND REINSTALL - [SDR IXXA08SMN124S](https://openairdocs.org/sdr/IXXA08SMN124S.md): Skin · misrepaired · Apr 17, 2008 · N602AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PART WITH IMPROPER REPAIR AT STATION XW -2.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. - [SDR IXXA08SMN123S](https://openairdocs.org/sdr/IXXA08SMN123S.md): Cargo Track · corroded · Apr 10, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 3 TRACK WITH CORROSION AT STATION 590.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED EXINTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK. FABRICATED SPLICES. - [SDR IXXA08SMN122S](https://openairdocs.org/sdr/IXXA08SMN122S.md): Cargo Track · worn · Apr 10, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 685.000. REMOVED EXISTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK AFT SIDE. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND REP - [SDR IXXA08SMN121S](https://openairdocs.org/sdr/IXXA08SMN121S.md): Cargo Track · worn · Apr 10, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 310.000 - 425.000. REMOVED DAMAGED SEGMENT OF TRACK AND EXISTING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXISTING SPLICES. INSTALLED SEGMENT OF NE - [SDR IXXA08SMN119S](https://openairdocs.org/sdr/IXXA08SMN119S.md): Skin · corroded · Mar 27, 2008 · N602AL · Doug DC873F · Fuselage Main, Plate/Skin > DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN LEFT SIDE WITH CORROSION AT STATION FS 850.000 LONGERON 24. REMOVED FASTENERS FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED ND - [SDR IXXA08SMN111S](https://openairdocs.org/sdr/IXXA08SMN111S.md): Skin · delaminated · Mar 27, 2008 · N602AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 225.000 TO STA XF 335.000. REMOVED AND REPLACED RIGHT WING NUMBER 4 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-20 - [SDR IXXA08SMN112S](https://openairdocs.org/sdr/IXXA08SMN112S.md): Skin · delaminated · Mar 27, 2008 · N602AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 5 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 345.000 TO STA XF 404.000. REMOVED AND REPLACED RIGHT WING NUMBER 5 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-20 - [SDR IXXA08SMN113S](https://openairdocs.org/sdr/IXXA08SMN113S.md): Skin · delaminated · Mar 27, 2008 · N602AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 6 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 415.000 TO STA XF 434.000. REMOVED AND REPLACED RIGHT WING NUMBER 6 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-20 - [SDR IXXA08SMN114S](https://openairdocs.org/sdr/IXXA08SMN114S.md): Skin Panel · delaminated · Mar 27, 2008 · N602AL · Doug DC873F · Spoilers > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 SPOILER PANEL DELAMINATED BETWEEN STATION XRS 247.000 TO XRS 351.000. ADJUSTED LEFT AND RIGHT WING GROUND FLIGHT SPOILER CABLES. PERFORMED OPS CHECK, GOOD TO SPOILER SYSTEM IAW DC8 MM 27-60-0 PAGE - [SDR IXXA08SMN120S](https://openairdocs.org/sdr/IXXA08SMN120S.md): Fitting · cracked · Mar 27, 2008 · N602AL · Doug DC873F · Wing, Landing Gear Attach Fittings > DURING ROUTINE C CHECK INSPECTION, FOUND RT MAIN LANDING GEAR WHEEL WELL FORWARD UPPER PART FITTING CRACKED AT STATION 857.125 AND STATION XCW 23.000. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK FOUND. CLEANED, TREA Next page: https://openairdocs.org/deregistered/N602AL-2014-05-29/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N602AL' AND deregistration_id = 'N602AL-2014-05-29' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N602AL-2014-05-29/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.